JPH0683864B2 - High rigidity core manufacturing method - Google Patents
High rigidity core manufacturing methodInfo
- Publication number
- JPH0683864B2 JPH0683864B2 JP60096670A JP9667085A JPH0683864B2 JP H0683864 B2 JPH0683864 B2 JP H0683864B2 JP 60096670 A JP60096670 A JP 60096670A JP 9667085 A JP9667085 A JP 9667085A JP H0683864 B2 JPH0683864 B2 JP H0683864B2
- Authority
- JP
- Japan
- Prior art keywords
- core
- protrusions
- mold
- die
- metal plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 14
- 239000002184 metal Substances 0.000 claims description 17
- 238000000034 method Methods 0.000 claims description 9
- 238000000465 moulding Methods 0.000 claims description 6
- 239000000463 material Substances 0.000 description 8
- 239000012530 fluid Substances 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 241000264877 Hippospongia communis Species 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 230000000452 restraining effect Effects 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
Landscapes
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Description
【発明の詳細な説明】 (産業上の利用分野) 本発明は高剛性のコアの製作方法に関し、詳くは高剛
性、高性能コアの製作を可能とする超塑性成形コアの新
しい製造方法に関するものである。Description: TECHNICAL FIELD The present invention relates to a method for producing a highly rigid core, and more particularly to a new method for producing a superplastically formed core that enables the production of a highly rigid and high performance core. It is a thing.
(従来の技術) 人工衛星の構体や機器取付用のパネルは軽量かつ高剛性
であることが要求され、従来からパネルのコアとして接
着ハニカムが使用されているが、高熱伝導及び高電気伝
導等の特性を要求されるパネルにおいては、コアとフエ
ーズプレートを金属接合することが必要となり、コアと
して超塑性成形体を使用することが試みられている。(Prior Art) Lightweight and highly rigid panels for satellite structures and equipment installations have been required, and bonded honeycombs have been used as the cores of panels for the past. In a panel that is required to have characteristics, it is necessary to metallically bond the core and the phase plate, and it has been attempted to use a superplastic molded body as the core.
従来の超塑性成形コアは、コア形状を刻んだ雄型の雌
型、いずれか一方に対してガス圧もしくは流体圧によつ
て超塑性金属板を成形することにより製作されている。
従来法による超塑性成形コアは、第3図(a)及び
(b)に示すように大きく2種類の形状に分類される。
すなわち第3図(a)のコルゲート形状と同図(b)の
交差コルゲート形状である。なお交差コルゲート形状に
ついてはコルゲート部分が成形される場合とその逆の部
分が成形される場合とがある。A conventional superplastic forming core is manufactured by forming a superplastic metal plate by a gas pressure or a fluid pressure in either one of a male type and a female type in which a core shape is carved.
Superplastic forming cores according to the conventional method are roughly classified into two types of shapes as shown in FIGS. 3 (a) and 3 (b).
That is, the corrugated shape in FIG. 3 (a) and the crossed corrugated shape in FIG. 3 (b). Regarding the cross corrugated shape, there are a case where the corrugated portion is formed and a case where the opposite portion is formed.
(発明が解決しようとする問題点) この従来の超塑性成形方法及び超塑性成形コアは次のよ
うな欠点を有している。(Problems to be Solved by the Invention) This conventional superplastic forming method and superplastic forming core have the following drawbacks.
(1) 成形に用いる型はコア形状をそのまま有してい
なければならず、型製作が高価であるとともに、連続し
た複曲面等の複雑形状を成形するための型は製作が困難
である。(1) The mold used for molding must have the core shape as it is, and it is expensive to manufacture the mold, and it is difficult to manufacture a mold for molding a complicated shape such as a continuous double curved surface.
(2) 型の凹部に対して超塑性金属板が一方向から張
出し成形されるため、成形部分でろ板厚減少が著しくな
り、超塑性成形コアの上面,下面の板厚が大幅に異な
る。(2) Since the superplastic metal plate is stretched and formed in one direction from the concave portion of the die, the thickness of the filter plate is remarkably reduced at the forming portion, and the plate thicknesses of the upper surface and the lower surface of the superplastic forming core are significantly different.
(3) コルゲート形状のコアはパネルの補強が一方向
に限られる。また交差コルゲート形状のコアはそれ自体
では剛性を有さないため、交差部分に剛性付与のための
別部品が必要となる。(3) In the corrugated core, the reinforcement of the panel is limited to one direction. Moreover, since the cross-corrugated core does not have rigidity by itself, a separate component is required to give rigidity to the intersection.
本発明者らは上記の欠点に鑑み、超塑性成形コアの製作
に際して、接合工程なしで(コア単体で)2方向以上の
強化方向を有し、かつコアの上下面で板厚分布を生じな
いような高剛性コアの形状及び成形方法を種々検討する
課程中において本発明を創案した。In view of the above-mentioned drawbacks, the present inventors have a strengthening direction of two or more directions without joining step (in a single core) when manufacturing a superplastic forming core, and do not generate a plate thickness distribution on the upper and lower surfaces of the core. The present invention was devised during the course of various studies on the shape and molding method of such a high-rigidity core.
(問題点を解決するための手段) 本発明は、交互にかつ規則的に配列された柱状突起部を
有する上型と下型で、超塑性状態にある金属板を挟み込
むようプレスして金属板の両面に張出成形を施す高剛性
コアの製作方法において、噛み合う位置における上記の
上型と下型の上記突起部の間隔が、上記金属板の板厚を
越える広さを有する上型と下型を用いて、上記金属板を
張出成形し、金属板の表裏に上記突起部に対応する先端
部と、該先端部と先端部の間に上記突起部の側面に接触
せずに形成される傾斜部を有するコアを製作することを
特徴とする高剛性コアの製作方法である。(Means for Solving the Problems) The present invention relates to an upper die and a lower die having columnar protrusions arranged alternately and regularly, and pressing a metal plate in a superplastic state by sandwiching the metal plate. In the method of manufacturing a high-rigidity core in which both surfaces of the upper mold are stretched, the distance between the protrusions of the upper mold and the lower mold at the meshing position is larger than the thickness of the metal plate. Using a mold, the metal plate is bulged, and formed on the front and back sides of the metal plate, corresponding to the projections, and between the tip and the tip without contacting the side surface of the projections. A method of manufacturing a high-rigidity core, which comprises manufacturing a core having an inclined portion.
本発明方法の具体的な一例を第1図(a)〜(b)に示
す。A specific example of the method of the present invention is shown in FIGS.
本発明の方法においては、上型と下型を用い第1図
(a)に示すように、図中白丸○であらわされる上型突
起部2と黒丸●であらわされる下型突起部3は、超塑性
特性を有する供試材1平面に対し、交互かつ規則的配列
となるような位置に設けられる。そして、上型と下型が
噛み合う位置において、上型と下型の柱状突起部の間隔
が被成形物である金属板の板厚より広くすることによ
り、上型の柱状突起部と下型柱状突起部の間に位置する
金属板は柱状突起部の側面と接触することなく変形され
てコアの傾斜部が形成される。以下第1図(a)のA−
A′断面を示す第1図(b)〜(d)を用いて説明す
る。In the method of the present invention, an upper mold and a lower mold are used, and as shown in FIG. 1 (a), the upper mold protrusion 2 represented by a white circle ○ and the lower mold protrusion 3 represented by a black circle are: They are provided at positions which are arranged alternately and regularly with respect to one plane of the test material having superplasticity. Then, at the position where the upper die and the lower die are engaged with each other, the gap between the columnar protrusions of the upper die and the lower die is made wider than the plate thickness of the metal plate which is the object to be molded, so that the columnar protrusions of the upper die and the lower die columnar The metal plate located between the protrusions is deformed without contacting the side surface of the columnar protrusion to form the inclined portion of the core. Hereinafter, A- in FIG.
This will be described with reference to FIGS. 1 (b) to (d) showing the A'section.
超塑性特性を有する供試材1は、交互にかつ規則的に配
列した突起部2,3を有する上型4及び下型5の間にセツ
トされ、周囲を押え治具6によつて拘束されている。上
型はプレス駆動軸7に直接つながれており、下型との平
行を保つたままゆつくりと駆動するようになつている。
これらの加工用治具の周囲には加熱用のヒータ8が配置
されている〔第1図(b)〕。供試材1はヒータ8によ
り超塑性を示す温度まで加熱され、その後上型4を供試
材1をはさみ込むように駆動することにより供試材1は
表裏両方向に交互に張出し成形され、金属板の表裏に上
型及び下型の柱状突起部に対応する先端部と、該先端部
と先端部の間に柱状突起部の側面に接触せずに形成され
る傾斜部を有する高剛性コアが製作される〔第1図
(c)及び(d)〕。The test material 1 having superplasticity is set between the upper die 4 and the lower die 5 having the protrusions 2 and 3 arranged alternately and regularly, and the periphery is restrained by the holding jig 6. ing. The upper die is directly connected to the press drive shaft 7, and is driven gently while keeping parallel with the lower die.
A heater 8 for heating is arranged around these processing jigs [FIG. 1 (b)]. The test material 1 is heated by the heater 8 to a temperature at which it exhibits superplasticity, and then the upper die 4 is driven so as to sandwich the test material 1 so that the test material 1 is alternately stretched in both front and back directions. A high-rigidity core having front and back surfaces of the plate corresponding to the columnar protrusions of the upper mold and the lower mold and an inclined portion formed between the tip and the tip without contacting a side surface of the columnar protrusion is provided. It is manufactured [Fig. 1 (c) and (d)].
上記の例で供試材拘束治具6は周囲部まで完全な張出し
成形するためのものであり、成形品の周囲をトリムして
利用する場合には特に必要ではない。また型の駆動方式
は、上記のプレス駆動の他にガス圧や流体圧による駆
動、あるいは歯車等による機械的な駆動のいずれを用い
てもよく、駆動する型は上型のみ、下型のみ、両方の型
のいずれの場合も供試材に対する型の相対位置は変わら
ないため、どの型を駆動してもかまわない。ヒータは型
の側面ではなく上下面に置いてもよく、また治具構成を
全て横置きとしてもかまわない。超塑性成形コアの特性
は、突起部の長さと間隔あるいは突起部の形状及び配列
を変えることによりコントロールすることが可能であ
る。たとえば第1図(a)の例は2方向を強化するよう
に突起部が配列しているが、第2図のように配列すると
3方向の強化が可能である。第2図中白丸〇は上型の突
起部位置を、黒丸●は下型の突起部位置を示す。In the above example, the test material restraining jig 6 is for completely stretch-molding up to the peripheral portion, and is not particularly necessary when trimming the periphery of the molded product for use. Further, the die driving system may use either gas pressure or fluid pressure driving, or mechanical driving such as gears in addition to the above press driving, and the driving die is only the upper die, only the lower die, In either case of the two molds, the relative position of the mold with respect to the test material does not change, so it does not matter which mold is driven. The heater may be placed on the upper and lower surfaces instead of the side surface of the mold, and the jig structure may be placed horizontally. The characteristics of the superplastic forming core can be controlled by changing the length and spacing of the protrusions or the shape and arrangement of the protrusions. For example, in the example of FIG. 1 (a), the projections are arranged so as to strengthen in two directions, but when arranged as shown in FIG. 2, strengthening in three directions is possible. In FIG. 2, a white circle ◯ indicates the position of the upper die protrusion, and a black circle ● indicates the lower die position.
(発明の効果) 本発明の方法は次のような特長を有する。(Effect of the Invention) The method of the present invention has the following features.
型は規則的に配列した突起部を有するだけであるた
め、従来の超塑性成形用の型に比べて安価である。Since the mold has only regularly arranged protrusions, it is cheaper than the conventional superplastic forming mold.
超塑性金属板は上下の型の突起部により表裏両方向
に張出し成形されるため、成形されたコアの板厚は上下
面で同じとなり、従来の超塑性成形コアのような板厚不
均一は生じない。Since the superplastic metal plate is formed by bulging in both front and back directions by the protrusions of the upper and lower molds, the thickness of the molded core is the same on the upper and lower surfaces, and the uneven thickness of conventional superplastic molded cores does not occur. Absent.
本発明方法によつて製作されるコアは、コア単体で
高い剛性を有し、かつ突起部の配列によつて強化方向を
2方向もしくは3方向とすることが可能である。The core manufactured by the method of the present invention has a high rigidity by itself, and the reinforcing direction can be set to two or three directions depending on the arrangement of the protrusions.
したがつて本発明の方法の軽量、高強度、高剛性を必要
とする全てのパネル構造のコアもしくはパネル本体の成
形法として適用できる。本発明は得られるコアが一枚の
板から成形されたコアであり、かつフエース・プレート
との接合部分が面であるため金属接合が容易であるので
高熱伝導,高電気伝導等の特性を要求されるパネルのコ
アの製造方法として適用可能である。Therefore, the method of the present invention can be applied as a molding method for cores or panel bodies of all panel structures that require light weight, high strength, and high rigidity. According to the present invention, the obtained core is a core formed from a single plate, and since the joint portion with the face plate is a surface, metal joining is easy, so that characteristics such as high heat conduction and high electric conduction are required. It is applicable as a manufacturing method of the core of the panel.
第1図(a)〜(d)は本発明の実施態様を説明する図
であつて、第1図(a)は上型および下型の突起部の位
置関係を示す図、同図(b)〜(d)は同図(a)のA
−A′断面相当部分を例にして、同図(b)は供試材セ
ツト状態、同図(c)はプレス途中の状態、同図(d)
はプレス終了状態を示す図である。 第2図は本発明の別の実施態様における上型および下型
の突起部の位置関係を示す図である。 第3図(a)および(b)は従来の超塑性成形コアを例
示する図で、同図(a)はコルゲート形状を、同図
(b)は交差コルゲート形状を示す。FIGS. 1 (a) to 1 (d) are views for explaining an embodiment of the present invention, and FIG. 1 (a) is a view showing the positional relationship between upper and lower mold projections, and FIG. ) To (d) are A in FIG.
Taking the part corresponding to the -A 'cross-section as an example, Fig. 7 (b) shows the test material in the set state, Fig. 6 (c) shows the state in the middle of pressing, and Fig. 6 (d).
[Fig. 6] is a view showing a pressed state. FIG. 2 is a view showing a positional relationship between upper and lower projections in another embodiment of the present invention. 3 (a) and 3 (b) are views illustrating a conventional superplastic forming core, in which FIG. 3 (a) shows a corrugated shape and FIG. 3 (b) shows a crossed corrugated shape.
───────────────────────────────────────────────────── フロントページの続き (72)発明者 浅田 正一郎 愛知県名古屋市港区大江町10番地 三菱重 工業株式会社名古屋航空機製作所内 (56)参考文献 特開 昭46−7095(JP,A) ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Shoichiro Asada 10 Oe-machi, Minato-ku, Nagoya, Aichi Mitsubishi Heavy Industries, Ltd., Nagoya Aircraft Manufacturing Co., Ltd. (56) Reference JP-A-46-7095 (JP, A)
Claims (1)
を有する上型と下型で、超塑性状態にある金属板を挟み
込むようプレスして金属板の両面に張出成形を施す高剛
性コアの製作方法において、噛み合う位置における上記
の上型と下型の上記突起部の間隔が、上記金属板の板厚
を越える広さを有する上型と下型を用いて、上記金属板
を張出成形し、金属板の表裏に上記突起部に対応する先
端部と、該先端部と先端部の間に上記突起部の側面に接
触せずに形成される傾斜部を有するコアを製作すること
を特徴とする高剛性コアの製作方法。1. A high die for forming a metal sheet in a superplastic state by sandwiching a metal sheet in a superplastic state with an upper die and a lower die having columnar protrusions arranged alternately and regularly to form a bulge on both sides of the metal sheet. In the method of manufacturing a rigid core, the metal plate is formed by using an upper mold and a lower mold in which the distance between the protrusions of the upper mold and the lower mold at the meshing position is larger than the thickness of the metal plate. Protrusion molding is performed to manufacture a core having front and back surfaces of the metal plate, which have tip portions corresponding to the protrusions, and inclined portions formed between the tip portions and the tip portions without contacting side surfaces of the protrusions. A method for manufacturing a high-rigidity core, which is characterized in that
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60096670A JPH0683864B2 (en) | 1985-05-09 | 1985-05-09 | High rigidity core manufacturing method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60096670A JPH0683864B2 (en) | 1985-05-09 | 1985-05-09 | High rigidity core manufacturing method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS61255728A JPS61255728A (en) | 1986-11-13 |
| JPH0683864B2 true JPH0683864B2 (en) | 1994-10-26 |
Family
ID=14171240
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP60096670A Expired - Lifetime JPH0683864B2 (en) | 1985-05-09 | 1985-05-09 | High rigidity core manufacturing method |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0683864B2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06226889A (en) * | 1993-02-05 | 1994-08-16 | Sky Alum Co Ltd | Panel material and composite panel using the same |
| CA2755463C (en) * | 2009-04-01 | 2014-07-08 | Autoneum Technologies Ag | Structured metal heat shield |
-
1985
- 1985-05-09 JP JP60096670A patent/JPH0683864B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS61255728A (en) | 1986-11-13 |
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